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RD-3A


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RD-3A Glushko LOx/Alcohol rocket engine. R-3A. Out of Production. Project for R-3A experimental missile. Stopped in favor of RD-103.

AKA: RD-102?. Status: Out of Production. Date: 1951-53. Thrust: 390.00 kN (87,670 lbf). Unfuelled mass: 885 kg (1,951 lb). Specific impulse: 214 s. Specific impulse sea level: 214 s. Height: 3.12 m (10.24 ft).

Thrust (sl): 390.000 kN (87,670 lbf). Engine: 885 kg (1,951 lb). Propellant Formulation: Lox/Alcohol-96%. Oxidizer to Fuel Ratio: 0.

Country: Russia. Launch Vehicles: R-3A. Propellants: Lox/Alcohol. Agency: Glushko bureau. Bibliography: 21, 283. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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